EP2189646A3 - Variable pitch rotor arrangement in a gas turbine engine - Google Patents
Variable pitch rotor arrangement in a gas turbine engine Download PDFInfo
- Publication number
- EP2189646A3 EP2189646A3 EP09252354.7A EP09252354A EP2189646A3 EP 2189646 A3 EP2189646 A3 EP 2189646A3 EP 09252354 A EP09252354 A EP 09252354A EP 2189646 A3 EP2189646 A3 EP 2189646A3
- Authority
- EP
- European Patent Office
- Prior art keywords
- rotor
- gas turbine
- turbine engine
- blades
- variable pitch
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 239000012530 fluid Substances 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/025—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the by-pass flow being at least partly used to create an independent thrust component
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/30—Blade pitch-changing mechanisms
- B64C11/38—Blade pitch-changing mechanisms fluid, e.g. hydraulic
- B64C11/385—Blade pitch-changing mechanisms fluid, e.g. hydraulic comprising feathering, braking or stopping systems
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/30—Blade pitch-changing mechanisms
- B64C11/38—Blade pitch-changing mechanisms fluid, e.g. hydraulic
- B64C11/40—Blade pitch-changing mechanisms fluid, e.g. hydraulic automatic
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/46—Arrangements of, or constructional features peculiar to, multiple propellers
- B64C11/48—Units of two or more coaxial propellers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/026—Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/70—Adjusting of angle of incidence or attack of rotating blades
- F05D2260/76—Adjusting of angle of incidence or attack of rotating blades the adjusting mechanism using auxiliary power sources
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Turbines (AREA)
Abstract
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB0821239.1A GB0821239D0 (en) | 2008-11-21 | 2008-11-21 | A machine such as a gas turbine |
Publications (3)
Publication Number | Publication Date |
---|---|
EP2189646A2 EP2189646A2 (en) | 2010-05-26 |
EP2189646A3 true EP2189646A3 (en) | 2017-11-15 |
EP2189646B1 EP2189646B1 (en) | 2019-01-09 |
Family
ID=40230579
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP09252354.7A Active EP2189646B1 (en) | 2008-11-21 | 2009-10-02 | Variable pitch rotor arrangement in a gas turbine engine |
Country Status (3)
Country | Link |
---|---|
US (1) | US8651812B2 (en) |
EP (1) | EP2189646B1 (en) |
GB (1) | GB0821239D0 (en) |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB201000103D0 (en) * | 2010-01-06 | 2010-02-17 | Rolls Royce Plc | Back-Up Feathers |
GB201007063D0 (en) | 2010-04-28 | 2010-06-09 | Rolls Royce Plc | A gas turbine engine |
GB201007564D0 (en) | 2010-05-06 | 2010-06-23 | Rolls Royce Plc | Back-up featherer |
GB201007569D0 (en) | 2010-05-06 | 2010-06-23 | Rolls Royce Plc | Pitch control mechanism |
GB201007567D0 (en) | 2010-05-06 | 2010-06-23 | Rolls Royce Plc | BAck-up featherer |
GB201007565D0 (en) | 2010-05-06 | 2010-06-23 | Rolls Royce Plc | Pitch control mechanism |
US9452831B2 (en) | 2013-04-22 | 2016-09-27 | Sikorsky Aircraft Corporation | Integration of rotary electrical actuator for swashplateless individual blade control |
US9334847B2 (en) | 2013-12-23 | 2016-05-10 | Grover Curtis Harris | Bi-rotational generator |
US10577080B2 (en) * | 2017-08-23 | 2020-03-03 | Hamilton Sundstrand Corporation | Dual valve systems for actuator control |
US11364990B2 (en) * | 2018-08-06 | 2022-06-21 | Pratt & Whitney Canada Corp. | Variable pitch propeller control system |
US11118464B2 (en) | 2018-10-11 | 2021-09-14 | General Electric Company | Aircraft gas turbine engine blade pitch change mechanism |
CN109573002A (en) * | 2018-12-12 | 2019-04-05 | 惠阳航空螺旋桨有限责任公司 | A kind of properller feathering pump |
IT201900003999A1 (en) | 2019-03-19 | 2020-09-19 | Ge Avio Srl | COMBINED CONTROL VALVE FOR OVER-SPEED, FLAG AND REVERSE ENABLING FOR A PROPELLER GROUP |
EP3763621B1 (en) | 2019-07-12 | 2024-08-28 | Ratier-Figeac SAS | Hydraulic actuation system |
US11097832B2 (en) | 2019-09-10 | 2021-08-24 | Hamilton Sundstrand Corporation | Dual actuator hydraulic pitch-lock propeller system |
FR3143001A1 (en) * | 2022-12-08 | 2024-06-14 | Safran Helicopter Engines | TURBOMACHINE MODULE EQUIPPED WITH A HYDRAULIC ACCUMULATOR AND TURBOMACHINE COMPRISING IT |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4878809A (en) * | 1988-07-05 | 1989-11-07 | Sundstrand Corporation | Power source and control mechanism for propeller pitch control |
WO1991009775A1 (en) * | 1989-12-26 | 1991-07-11 | United Technologies Corporation | Pitch control system |
US5282719A (en) * | 1991-05-13 | 1994-02-01 | Alliedsignal Inc. | Quad mode fan pitch actuation system for a gas turbine engine |
US5897293A (en) * | 1996-11-22 | 1999-04-27 | United Technologies Corporation | Counterweighted propeller control system |
US20030180146A1 (en) * | 2002-03-19 | 2003-09-25 | Arel David V. | Actuation system for a controllable pitch propeller |
US20050135929A1 (en) * | 2003-12-19 | 2005-06-23 | Pratt & Whitney Canada Corp. | Pressurized oil supply for propeller engine system |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4352634A (en) | 1980-03-17 | 1982-10-05 | United Technologies Corporation | Wind turbine blade pitch control system |
US4348155A (en) | 1980-03-17 | 1982-09-07 | United Technologies Corporation | Wind turbine blade pitch control system |
US4379678A (en) * | 1980-10-07 | 1983-04-12 | Textron, Inc. | Individual blade control |
GB2151712B (en) | 1983-12-19 | 1987-10-28 | Sundstrand Corp | Ram air turbine |
US4555219A (en) * | 1984-08-23 | 1985-11-26 | United Technologies Corporation | Hub-mounted actuators for blade pitch collective control |
US4936746A (en) * | 1988-10-18 | 1990-06-26 | United Technologies Corporation | Counter-rotation pitch change system |
US4948339A (en) | 1989-01-23 | 1990-08-14 | General Electric Company | Propeller blade counterweight |
US5242265A (en) * | 1990-07-23 | 1993-09-07 | General Electric Company | Aircraft pitch change mechanism |
US5213471A (en) * | 1990-09-04 | 1993-05-25 | General Electric Company | Propeller pitch control |
US5174718A (en) * | 1991-08-12 | 1992-12-29 | United Technologies Corporation | Blade pitch change control system |
US5183387A (en) * | 1992-01-03 | 1993-02-02 | Allied-Signal, Inc. | Fault-tolerant apparatus for controlling blade pitch |
US6422816B1 (en) * | 2001-05-21 | 2002-07-23 | Hamilton Sundstrand Corporation | Variable pitch propeller control system |
DE102006023411A1 (en) | 2006-05-17 | 2007-11-22 | Robert Bosch Gmbh | Rotor blade device for adjusting blade angle of rotor blade of wind turbine on rotor shaft, has two electro motor drive, in which primary has frequency converter and secondary has electro motor with standby energy storage |
EP2052965B1 (en) * | 2008-01-11 | 2013-05-15 | MT-Propeller Entwicklung GmbH | Hydraulic adjustable propeller |
-
2008
- 2008-11-21 GB GBGB0821239.1A patent/GB0821239D0/en not_active Ceased
-
2009
- 2009-10-02 US US12/588,084 patent/US8651812B2/en active Active
- 2009-10-02 EP EP09252354.7A patent/EP2189646B1/en active Active
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4878809A (en) * | 1988-07-05 | 1989-11-07 | Sundstrand Corporation | Power source and control mechanism for propeller pitch control |
WO1991009775A1 (en) * | 1989-12-26 | 1991-07-11 | United Technologies Corporation | Pitch control system |
US5282719A (en) * | 1991-05-13 | 1994-02-01 | Alliedsignal Inc. | Quad mode fan pitch actuation system for a gas turbine engine |
US5897293A (en) * | 1996-11-22 | 1999-04-27 | United Technologies Corporation | Counterweighted propeller control system |
US20030180146A1 (en) * | 2002-03-19 | 2003-09-25 | Arel David V. | Actuation system for a controllable pitch propeller |
US20050135929A1 (en) * | 2003-12-19 | 2005-06-23 | Pratt & Whitney Canada Corp. | Pressurized oil supply for propeller engine system |
Also Published As
Publication number | Publication date |
---|---|
US8651812B2 (en) | 2014-02-18 |
EP2189646A2 (en) | 2010-05-26 |
US20100129214A1 (en) | 2010-05-27 |
GB0821239D0 (en) | 2008-12-31 |
EP2189646B1 (en) | 2019-01-09 |
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